Abstract An integral method is proposed for calculating a jet propagating from the turbofan engine thrust reverser and interacting with a stream formed as a result of the after-landing aircraft run. The calculation results for the PS-90 engine are presented. The calculation data obtained show that the mathematical model developed adequately describes a qualitative pattern of main parameter variation in the sector jet propagating in a stream.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Integral method for calculating a turbofan engine thrust reverser jet interacting with an external stream


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    2010-06-01


    Format / Umfang :

    9 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch






    Aircraft engine thrust reverser

    Emerald Group Publishing | 1998


    Engine thrust reverser lock

    WILLETT KENNETH / MEARS JOHN STEPHEN / CONWAY GEORGE et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Engine Thrust Reverser Lock

    WILLETT KENNETH / MEARS JOHN STEPHEN / CONWAY GEORGE et al. | Europäisches Patentamt | 2015

    Freier Zugriff